Dr Markus J Kloker
University of Stuttgart
Lecturer, General Science & Engineering
My co-authors include
DNS of compressible turbulent boundary layers at varying subsonic Mach numbers
Effect of Upstream Flow Deformation Using Plasma Actuators on Crossflow Transition Indu...
Direct Numerical Simulation of Foreign-Gas Film Cooling in Supersonic Boundary-Layer Flow
Instability and transition mechanisms induced by skewed roughness elements in a high-sp...
Journal of Fluid Mechanics
Influence of Cooling-Gas Properties on Film-Cooling Effectiveness in Supersonic Flow
Journal of Spacecraft and Rockets
Plasma actuators for laminar flow control
Journal of Physics D Applied Physics
Swept-Wing Boundary-Layer Receptivity to Steady Free-Stream Disturbances
Effusion Cooling and Flow Tripping in Laminar Supersonic Boundary-Layer Flow